View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 3230U 68040B 25197.82275326 .00001766 00000-0 13987-3 0 9996
2 3230 74.0317 74.8509 0025837 315.0955 44.8142 15.01230757 75835
Epoch (UTC): | 16 July 2025 19:44:45 |
Eccentricity: | 0.0025837 |
inclination: | 74.0317° |
perigee height: | 545 km |
apogee height: | 581 km |
right ascension of ascending node: | 74.8509° |
argument of perigee: | 315.0955° |
revolutions per day: | 15.01230757 |
mean anomaly at epoch: | 44.8142° |
orbit number at epoch: | 7583 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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